N797FD

Service difficulty reports · 113

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N797FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202208222026Plate · crackedRIGHT WING TRAILING EDGE WIGGLE PLATE AT WS 342 IS CRACKED REMOVED & REPLACED WIGGLE PLATES AT RIGHT WING TRAILING EDGE WS 342 IAW BAC DWG 113N1630, REV -Aug 22, 2022 · N797FD · Boeing 757222 · Wing Main, Frame StructureSDR FDEA202208222025Angle · crackedEXT FUSELAGE AFT OF R/M/G WHEEL WELL ATTACH ANGLE CRACKED BS 1180, BL 11R REMOVED & REPLACED ANGLE IAW BAC DWG 149N7528, REVISION J, & B757 SRM 51-40-02Aug 22, 2022 · N797FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA202208181998Support · crackedRMLG WHEEL WELL, WING TO BODY SUPPORT SUB STRUCTURE CLIP IS CRACKED APPROX 8" UP FROM THE CORNER OF THE CUTOUT AT STA 1100 REMOVED & RPELACED SUPPORT IAW BAC DWG 149N7552, REVISION A & B757 SRM 51-40-02Aug 18, 2022 · N797FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202208101953Support Angle · crackedFORWARD CARGO BELOW AIR FILTER SUPPORT ANGLE IS CRACKED AT STA 850 REMOVED AND REPLACED WITH FABRICATED FORWARD PIT BELOW AIR FILTER SUPPORT ANGLE AT STA 850Aug 10, 2022 · N797FD · Boeing 757200 · Fuselage Miscellaneous StructureSDR FDEA202205281323Floorbeam · crackedSTA 580 STUB FLOOR BEAM L/H IS CRACKED UNDER SEAT TRACK AT LBL 45.5 REMOVED DAMAGED L/H STUB FLOOR BEAM AT STA 580 REF. 757 SRM 51-40-02. OK TO INSTALL STUB FLOOR BEAM AT STA 580 REF B757 SRM 51-40-02 May 28, 2022 · N797FD · Boeing 757200 · Fuselage Main, Floor BeamSDR FDEA202203220682Gust Lock · failedMDIS 797 52-10 6261 22MAR22 MEM FACT U L1 DOOR GUST LOCK CAM BROKEN MEL 22MAR22 05:05 MEM U RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 25MAR22 MEL 52-11-01-A: L1 DOOR INOP C/7309723 PART 22MAR22 05:05Mar 22, 2022 · N797FD · Boeing 757200 · Passenger/Crew DoorsSDR FDEA202109082248Slide · unwanted deployWHILE WORKING EO F-5200-E0320318 D PT2 L1 DOOR SLIDE DEPLOYED. RELEASED FOR SERVICE. L1 SLIDE MISSING. SLIDE STOWED BEHIND RCB DOOR BOTTLE WILL REQUIRE SERVICING. REMOVED AND REPLACED L1 DOOR SLIDE REF AMM 25-66-00-2.Sep 8, 2021 · N797FD · Boeing 757222 · Escape SlideSDR FDEA202108172026Slide · inoperativeWHEN CLOSING MAIN CABIN DOOR, SLIDE BLEW DOOR OPEN, BUT THE SLIDE DID NOT DEPLOY. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE. REF 757 MM 25-66-01-4.Aug 17, 2021 · N797FD · Boeing 757222 · Escape SlideSDR FDEA202108172044Slide · malfunctionedWHEN CLOSING MAIN CABIN DOOR, SLIDE BLEW DOOR OPEN BUT THE SLIDE DID NOT DEPLOY. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE. REF 757 MM 25-66-01-4.Aug 17, 2021 · N797FD · Boeing 757222 · Escape SlideSDR FDEA202010022400Slide · unwanted deployAFTER BLOCK IN, 1R DOOR SLIDE DEPLOYED WHEN GROUND CREW OPENED DOOR. INSTALLED NEW SLIDER ON GIRTBAR AND TARGET, IN REF TO 757 AMM 25-66-01-4. OPERATIONS CHECK DOOR ARM LIGHT IS GOOD.Oct 2, 2020 · N797FD · Boeing 757222 · Escape SlideSDR FDEA2020072761663Attach Angle · crackedLEFT LOWER SIDEWALL ATTACH ANGLE AT BS 640 CRACKED. REMOVED AND REPLACED THE ANGLE IAW DWG 453N1131 AND SRM 51-40-02.Jul 26, 2020 · N797FD · Boeing 757222 · Fuselage Main, Attach FittingsSDR FDEA2020072751649Battery Pack · failedEMERGENCY BATTERY PACK DOES NOT HOLD CHARGE. REMOVED, REPLACED, AND OPS CHEC KED GOOD EMERGENCY LIGHT BATTERY PACK M730 PER B757 AMM 33-51- 07-2.Jul 25, 2020 · N797FD · Boeing 757222 · Emergency LightingSDR FDEA2020072431635Bracket · crackedLEFT PYLON,UNDER PANEL 435AR FWD LOWER CORNER HAS BRACKET CRACKED REMOVED AND REPLACED ATTACH ANGLE PER B757 SRM 51-40-02 AND DWG #313N3052 REV BJul 23, 2020 · N797FD · Boeing 757222 · Nacelle/Pylon Miscellaneous StructureSDR FDEA202007211612Rivet · wrong partDURING AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR ON LEFT WING OUTBOARD MAIN FLAP LEADING EDGE SKIN DOES NOT MEET CURRENT SRM STANDARDS DUE TO INCORRECT RIVET SPACING,CUTOUT ORIENTATION,AND REPAIR PARTS USEDJul 21, 2020 · N797FD · Boeing 757222 · Wing StructureSDR FDEA2020072311603Seat Track · corrodedMAIN CABIN, FWD RIGHT WET AREA, SEAT TRACK CORRODED BS 365 - 377 RBL 45 COMPLIED WITH EA F-5310-T0355330.Jul 21, 2020 · N797FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202007211610Seat Track · corrodedMAIN CABIN, FWD L/H WET AREA, LBL7 SEAT TRACK CORRODED TAPED AREAS ON SIDE OF TRACK 345 - 379 REMOVED CORROSION, ORIGINAL THICKNESS .072" MATERIAL REMOVED .018", REMAINING .054", OUT OF LIMITS OF B757 SRM 53-10-52-01, FABRICATED SEAT TRACK IAW VENTURA Jul 21, 2020 · N797FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202007201587Plate · corrodedMAIN CABIN, FWD RT WET AREA, CORROSION AT O2 LINE FEED THROUGH BS 375, RBL 37. REMOVED O2 LINE IAW AMM 53-11-00-2 & 20-11-00-2. REMOVED O2 PLATE IAW SRM 51-40-02. FABRICATED A NEW O2 PLATE IAW DWG 3516, REV -. INSTALLED THE NEW O2 PLATE IAW DWG 3516 REV - &Jul 20, 2020 · N797FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA2020072301587Line · corrodedMAIN CABIN, FWD RT WET AREA, CORROSION AT O2 LINE FEED THROUGH STA 375 RBL 37 REMOVED O2 LINE IAW AMM 53-11-00-2 AND 20-11-00-2. REMOVED O2 PLATE IAW SRM 51-40- 02. FABRICATED NEW O2 PLATE IAW DWG 3516 REV -. INSTALLED NEW O2 PLATE IAW DWG 3516 REV - AND SRM Jul 20, 2020 · N797FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA2020072391584Bracket · crackedR/H PYLON PANEL O/B INSIDE PANEL 445BR BRACKET FOR CONDUIT CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 313N3033 REV D AND B757 SRM 51-40-02Jul 19, 2020 · N797FD · Boeing 757222 · Nacelle/Pylon, Attach FittingsSDR FDEA202007191583Bracket · crackedR/H PYLON I/B PANEL 445AL CONDUIT INSIDE FWD BRACKET CRACKED REMOVED AND REPLACED BRACKET PER BOEING DWG # 313N3053 REV E AND SRM 51-40-02Jul 19, 2020 · N797FD · Boeing 757222 · Nacelle/Pylon, Attach FittingsSDR FDEA202007171569Nut Plate · corrodedMAIN CABIN, FWD R/H WET AREA, FLOOR BAEM CORRODED AT NUT PLATES STA 325 RBL 35-58 REMOVED CORROSION ORIGINAL THICKNESS .120 REMOVED .011 NEW THICKNESS .109 WICH IS FOUND TO BE WITHIN LIMITS WICH IS FOUND TO BE WITHIN LIMITS IAW B757 SRM 53-10-08-1A AND BOEJul 17, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA202007171568Seat Track · corrodedMAIN CABIN, FWD RT WET AREA HAD CORROSION ON THE SEAT TRACK, BS 365 - 379, RBL 25. REMOVED CORROSION, ORIGINAL THICKNESS .070, REMOVED MATERIAL .009, REMAINING .061 FOUND WITHIN LIMITS IAW SRM 53-00-52--1A, DETAIL 7, DWG 1520- 792 AND SRM 53-10-52-01,Jul 17, 2020 · N797FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202007171566Skin · puncturedLEFT HORIZONTAL STAB LOWER SURFACE SKIN WAS A PUNCTURED APPROX. 5 INCHES LONG, APPROX. 5 INCHES FROM THE LEADING EDGE. REPAIRED HORIZONTAL STAB LOWER SKIN BY REMOVING DAMAGE, LAYING UP CORE PLUG AND EXT. DOUBLER REPAIR AND CURED IAW SRM 55-10-01 AND SRM 51Jul 17, 2020 · N797FD · Boeing 757222 · Horizontal Stabilizer, Plate/SkinSDR FDEA202007161533Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8 LBL 4. REMOVED AND REPLACED FLOOR BEAM LOWER NUTPLATE STRIP AT BS 1681.8 LBL 4, IAW FEDEX B757 SRM 51-40-02 AND DWG 146N5693 REV C.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA2020072361532Floorbeam · corrodedFLOOR BEAM LOWER NUT PLATE STRIP IS CORRODED BS 1681.8, LBL39 REMOVED AND REPLACED FLOOR BEAM LWR NUTPLATE STRIP AT BS 1681.8 LBL 39 IAW SRM 51-40-02 AND DWG 146N5693 REV CJul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA202007161542Floorbeam · corrodedMAIN CABIN, FWD RIGHT WET AREA , PRIOR TEE CAP REPAIR HAS CORROSION AT SEAT TRACK AREAS, BS 365 BL 0 TO RBL 64. REMOVED CORROSION, ORIGINAL THICKNESS (.125") REMOVED (.005") REMAINING (.120") CROSSECTIONAL AREA IS LESS THAN 5% WITH A1=.250" AND A2= .0025Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA2020071761541Floor Support · corrodedFLOOR SUPPORT FITTING UPPER SURFACE IS CORRODED BS 1661.8 - BS 1681.8, RBL 0. REMOVED AND REPLACED CORRODED CHANNEL IAW DWG 146N5576 AND SRM 51-40-03-06, FID 1 SHEET 4 AND SHEET 7.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA2020071761540Pressure Deck · corrodedMAIN CABIN PRESSURE DECK UPPER PLATE IS CORRODED BS 1714, LBL 6 - BL9 REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 514-20-01.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA2020071761536Pressure Deck · corrodedMAIN CABIN PRESSURE DECK UPPER PLATE WAS CORRODED, BS 1685.8 - BS 1688.5. REMOVED THE CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA2020071761535Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED AT SEVERAL AREAS, BS 1681.8, LBL 4 - LBL 47. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA2020071761534Floorbeam · corrodedFLOORBEAM UPPER SURFACE WAS CORRODED, BS 1681.8, RBL 11. REMOVED CORROSION IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53- 60-51-1A, TREATED BARE METAL IAW SRM 51-20-01.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA2020071761532Nut Plate · corrodedFLOORBEAM LOWER NUT PLATE STRIP WAS CORRODED, BS 1681.8, LBL 39. REMOVED AND REPLACED THE FLOORBEAM LWR NUTPLATE STRIP IAW SRM 51-40-02, AND DWG 146N5693, REV C.Jul 16, 2020 · N797FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA2018110213075Ball Screw · corrodedTE FLAP DISAGREE WHEN FLAP HANDLE WAS MOVED FROM 0 TO 1. RAN QRH AND LANDED. R & R THE LT INBD NR 4 FLAP TRANSMISSION ASSY IAW MM 27-51-06-4, UP TO UNIVERSAL JOINT DRIVE SHAFT. FOUND THE DRIVE SHAFT BEARINGS EXCESSIVELY CORRODED AND UNSERVICEABLE. R & R Nov 1, 2018 · N797FD · Boeing 757222 · Trailing Edge Flap Control SystemSDR FDEA2018091422462Cylinder · dischargedL1 DOOR ASSIST BOTTLE DISCHARGED UPON DOOR DE-ACTIVATION. R&R LT EMERG DOOR ASSIST CYL PER AMM 52-11-30-4. AC OK FOR SERVICE.Sep 12, 2018 · N797FD · Boeing 757222 · Emergency ExitsSDR FDEA2018081752031Skin · damagedFUSELAGE SKIN AT BS 1787.45, STRINGERS 17R-18R HAD A 6 INCH SCRATCH BELOW THE FAIRING. REMOVED THE DAMAGED, FABRICATED, AND INSTALLED A REPAIR IAW SRM 53-80-70-2R, FIG 201, REP 2 DETAIL I.Aug 15, 2018 · N797FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201610283741Transmitter · inoperativeAFTER TAKEOFF, WHEN FLAP HANDLE WAS MOVED FROM 5 TO 1 DEGREES, AN IMMEDIATE EICAS MESSAGE FOR TE FLAP ASYMETERY APPEARED AND THE FLAP GUAGE STOPPED SLIGHTLY LESS THAN 5 DEGREES WITH ASSOCIATED FLAP STOPPAGE. REMOVED AND REPLACED THE FLAP POSITION TRANSMITTOct 28, 2016 · N797FD · Boeing 757222 · Trailing Flap Position Indicating SystemSDR FDEA201609153264Handle · looseCAPTAIN`S SLIDING WINDOW WILL NOT LOCK IN CLOSED POSITION. FOUND CAPTAIN'S SLIDING WINDOW HANDLE LOOSE CAUSING LOCK FEATURE TO BE INOPERABLE. RESECURED HANDLE INTO POSITION. WINDOW OPERATES NORMAL IAW MM 56-11-02-5-0.Sep 15, 2016 · N797FD · Boeing 757222 · Flight Compartment WindowsSDR FDEA201608032789Door Frame · gougedFWD E & E CUT OUT FWD DOOR FRAME GOUGED BY DOOR LOCK PIN. COMPLIED WITH EA F-5310-T0327174. BS 231.25, BL0 FRAME DENT, REPAIR. THIS IS A MAJOR REPAIR. PERFORMED SATISFACTORY. OPS CHECK FORWARD ELECTRONIC EQUIPMENT DOOR SENSOR IAW AMM 52-71-00-5.Aug 3, 2016 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201502140532Wire · damagedCOCKPIT EMER LIGHT INOPERATIVE. REWIRED IAW WDM CH 33-51-12. OPERATIONS CHECKED NORMAL.Feb 14, 2015 · N797FD · Boeing 757222 · Light System WiringSDR FDEA201411043505Power Supply · malfunctionedON SERVICE CHECK FOUND FLIGHT DECK EMER LIGHT NOT WORKING. DISCONNECTED THE FWD & AFT EMER LIGHTING POWER SUPPLIES & THEN RECONNECTED BOTH. ACFT WAS POWERED UP FOR APPROX 2 HRS, THEN RAN THE POWER SUPPLY TEST ON EACH IAW MM 33-51-07-02. BOTH POWER SUPPLIES Nov 4, 2014 · N797FD · Boeing 757222 · Emergency LightingSDR FDEA201408222292Skin · dentedPREVIOUS OPERATOR INCOMING DENT, 3 EACH. DENTS AT BS 760 DIRECTLY ABOVE & BELOW STRINGER 16LT. FUSELAGE SKIN REPAIR AT STATION 780 BETWEEN STRINGER 15L - 17L WAS ACCOMPLISHED, DUE TO EFFECTING THE PTF CONVERSION ON EA 757-5331-16-F4651 REV DATED JULY 30, 2Aug 22, 2014 · N797FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201407312025Skin · gougedLEFT WING OTBD MAIN FLAP UPPER SURFACE LE GOUGED. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 57-53-01 FIG 101 DETAIL VI. REPAIRED & INSTALLED FILLER & DOUBLER IAW SRM 57-53-01 FIG 201 REPAIR 2. MAJOR REPAIR.Jul 31, 2014 · N797FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201407312020Gate · corrodedR1 DOOR LOWER GATE LOWER END HAS CORROSION. ENTERED IN ERROR.Jul 31, 2014 · N797FD · Boeing 757222 · Service DoorsSDR FDEA201407091677Crease Beam · corrodedCORROSION AT CABIN CREASE BEAM INNER CHORD STATION 730, BY DOOR L2. ORIGINAL CREASE BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, FIG 101, DETAIL IV. R & R CREASE BEAM SECTION IAW SRM 51-40-02, PG 1, SRM 51-40-05 & DWG 143N8322, BS 686 - 760, LBL 58. MAJJul 9, 2014 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201406201497Frame · gougedAFT CARGO BAY, BS 1480 STRINGER 23R FRAME INBD FLANGE GOUGED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, DETAIL II. REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1030. MAJOR REPAIR.Jun 20, 2014 · N797FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201406191491Skin · gougedRIGHT WING OTBD FWD FLAP OTBD LE UPPER SURFACE GOUGED AFTER REMOVED DAMAGE CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 57-53-01 PG 106 FIG 101 DETAIL VI. R & R LE IAW SRM 51-40-02 & DWG 113N3500 AT RT WING OTBD FWD FLAP.Jun 19, 2014 · N797FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201406171483Frame · dentedAFT CARGO BAY BS 1420 STRINGER 24L, FRAME INBD FLANGE AT SPLICE DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG. 101, PG. 1. REMOVED AND REPLACED FRAME S13 - 24L IAW SRM 51-40-02 AND DRAWING 146N1028. MAJOR REPAIR.Jun 17, 2014 · N797FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201406171481Frame · dentedAFT PIT BS 1320 STRINGER 25R TO 26R FRAME INBD FLANGE, DENTED FRAME. DENT IS OUT OF LIMITS IAW SRM 53-00-07 FIG 101 DETAIL I. R & R FRAME BS 1320, STRINGER 24R - 24L IAW SRM 51-40-02 & DWG 146N1028. MAJOR REPAIR.Jun 17, 2014 · N797FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201406161468Crease Beam · corrodedCORROSION ON CREASE BEAM INNER CHORD STATION 377 BY DOOR L1. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13 FIG 101 DETAIL II. R & R WITH NEW CREASE BEAM AT STATION 395 - 324 LBL 61 IAW SRM 51-40-02 & DWG 657N3383 MAJOR REPAIR.Jun 16, 2014 · N797FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201406021282Skin · chafedR4 DOOR INBD SKIN DOUBLER CHAFED.Jun 2, 2014 · N797FD · Boeing 757222 · Service Doors
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